Experimental study on compression properties and failure mechanism of 3D MWK carbon/epoxy composites at elevated temperatures

2017 ◽  
Vol 39 (S4) ◽  
pp. E1987-E1999 ◽  
Author(s):  
Nan Jiang ◽  
Dian-Sen Li ◽  
Qian-qian Yao ◽  
Hong-wei Duan ◽  
Frank Ko
Keyword(s):  
Experimental Study ◽  
Failure Mechanism ◽  
Elevated Temperatures ◽  
Epoxy Composites ◽  
Compression Properties

Experimental study on the mechanical behavior and failure mechanism of 3d MWK carbon/epoxy composites under quasi-static loading

2015 ◽  
Vol 37 (12) ◽  
pp. 3486-3498 ◽  
Author(s):  
Dian-Sen Li ◽  
Yong Xia ◽  
Qing Zhou ◽  
Lei Jiang ◽  
Nan Jiang
Keyword(s):  
Experimental Study ◽  
Mechanical Behavior ◽  
Failure Mechanism ◽  
Static Loading ◽  
Epoxy Composites

Experimental study on the compression properties and failure mechanism of 3D integrated woven spacer composites

2014 ◽  
Vol 56 ◽  
pp. 50-59 ◽  
Author(s):  
Chuang-Qi Zhao ◽  
Dian-Sen Li ◽  
Tian-Qi Ge ◽  
Lei Jiang ◽  
Nan Jiang
Keyword(s):  
Experimental Study ◽  
Failure Mechanism ◽  
Compression Properties

Temperature effects on the compression behavior and failure of 3-D MWK glass fabric-reinforced epoxy composites

2018 ◽  
Vol 31 (4) ◽  
pp. 449-461 ◽  
Author(s):  
Dian-sen Li ◽  
Zhuo Wang ◽  
Hong-wei Duan ◽  
Lei Jiang
Keyword(s):  
Temperature Effects ◽  
Elevated Temperatures ◽  
Epoxy Composites ◽  
Glass Fabric ◽  
Fiber Architecture ◽  
Compression Behavior ◽  
Compression Properties ◽  
Out Of Plane ◽  
Plane Compression ◽  
Loading Modes

This article reports the temperature effects on the in-plane and out-of-plane compression behavior and failure of 3-D multiaxial warp-knitted glass fabric-reinforced epoxy composites. The damage and fracture morphology are observed from macroscopic and microscopic views, and the failure mechanism is demonstrated. The results show that the temperature has significant effect on in-plane and out-of-plane compression properties, the stress versus strain curves decline, and the properties decrease significantly with increasing the temperature. The temperature of 75°C is a key point, at which change in compression properties occurs, and at 150°C, the materials become plastic. Moreover, fiber architecture and loading modes are also important factors on compression properties of composites. The results also show that the damage and failure patterns vary with temperature, fiber architecture, and loading modes. Under in-plane compression, material A shows local 0° fiber layers delaminating and becomes softening and plasticity with increasing temperature. Material B shows delaminating between 0°, 90°, +45°, and −45° fiber layers along 45° angle and exhibits multiple delaminating at elevated temperatures. Under out-of-plane compression, material A shows multiple local shear fracture with 45° angle and experiences softening, roughness, and expansion at elevated temperatures. Material B exhibits shear brittle failure clearly, and delaminating dominates the main failure with increasing the temperature.

Experimental Study on the Short-Circuit Failure Mechanism of Cumulative Discharge in Gas Discharge Tube

2020 ◽  
pp. 1-8
Author(s):  
Lingyun Cheng ◽  
Weijiang Chen ◽  
Nianwen Xiang ◽  
Kejie Li ◽  
Kai Bian ◽  
...  
Keyword(s):  
Experimental Study ◽  
Failure Mechanism ◽  
Discharge Tube ◽  
Short Circuit ◽  
Gas Discharge

Fracture toughness and failure mechanism of graphene based epoxy composites

2014 ◽  
Vol 97 ◽  
pp. 90-99 ◽  
Author(s):  
Swetha Chandrasekaran ◽  
Narumichi Sato ◽  
Folke Tölle ◽  
Rolf Mülhaupt ◽  
Bodo Fiedler ◽  
...  
Keyword(s):  
Fracture Toughness ◽  
Failure Mechanism ◽  
Epoxy Composites
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